Collision with terrain – 7 km north-north-west of Hornsby, New South Wales, on 1 March 2008

Summary

On 1 March 2008, at about 1300 Eastern Daylight-saving Time the pilot of a Bell Helicopter 206B Jetranger III was flying over a property on a private flight with four passengers. Witnesses reported seeing the helicopter flying over the property at about 100 ft above ground level. At the completion of one pass, the helicopter was observed by witnesses on the ground to bank steeply to the left, roll out and descend into surrounding trees. The helicopter impacted the trees and was seriously damaged. One of the occupants was discovered outside the helicopter and all sustained serious injuries.

Examination of the wreckage did not indicate any mechanical defects that would have affected the safe operation of the helicopter.

Occurrence summary

Investigation number AO-2008-017
Occurrence date 01/03/2008
Location 7 km NNW, Hornsby
State New South Wales
Report release date 03/10/2008
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Collision with terrain
Occurrence class Accident
Highest injury level Serious

Aircraft details

Manufacturer Bell Helicopter Co
Model 206
Registration VH-NBP
Serial number 4185
Sector Helicopter
Operation type Private
Damage Destroyed

Fumes Event, VH-EBY, 275 km west-south-west of Sydney, New South Wales, on 25 February 2008

Summary

On 25 February 2008, at about 2128 Eastern Daylight-saving Time, the flight crew of a Boeing Company 747-338 (747) aircraft, registered VH-EBY, detected a smell that slowly increased in intensity. At that time, the aircraft was cruising at 37,000 ft and was about 275 km west south-west of Sydney, NSW.

The flight crew donned their emergency oxygen equipment and transmitted a PAN call to air traffic control. The aircraft was cleared direct to Sydney for landing and was escorted to the terminal by the airport fire services for disembarkation.

An inspection by the operator determined that loose terminal connections to the left windshield heat element resulted in electrical arcing and fumes on the flight deck.

The aircraft manufacturer has a programme to replace the windshields in the 747 with an enhanced windshield heater wiring connection that should address the risk of electrical arcing in that component.

Occurrence summary

Investigation number AO-2008-013
Occurrence date 25/02/2008
Location CULIN NSW, 270 degrees/93 km
State New South Wales
Report release date 29/05/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Fumes
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 747
Registration VH-EBY
Serial number 23823
Sector Jet
Operation type Air Transport High Capacity
Departure point Perth, WA
Destination Sydney, NSW
Damage Nil

Mid-air collision - 10 km north-east of Wee Waa, New South Wales, on 26 February 2008

Preliminary report

Preliminary report released 11 June 2008

At 0930 Eastern Daylight-saving Time on 26 February 2008, Air Tractor Inc. 502 registered VH-CJK (CJK), whose pilot was engaged in the aerial spraying of a field approximately 10 km NE of Wee Waa township, NSW, and Air Tractor Inc. 502B registered VH-ATB (ATB), that had just departed from an airstrip approximately 13 km north-east of Wee Waa, collided. The pilot of CJK was fatally injured and the aircraft destroyed by collision forces with the other aircraft and by ground impact. It did not catch fire. The pilot of ATB was seriously injured and the aircraft destroyed by collision forces with the other aircraft, ground impact, and a post impact fire.

Summary

At about 0930 Eastern Daylight-saving Time on 26 February 2008, an Air Tractor Inc. 502, registered VH-CJK (CJK) that was aerial spraying 10 km north-east of Wee Waa, New South Wales and an Air Tractor Inc. 502B, registered VH-ATB (ATB) that had just departed from a nearby airstrip, collided at about 200 ft above ground level. The pilot of CJK was fatally injured and the pilot of ATB was seriously injured. Both aircraft were seriously damaged. Neither pilot was aware of the other aircraft and, although visibility at the time of the accident was reported as 'good', either one or both pilots did not see the other aircraft in sufficient time to avoid a collision.

The limitations of an unalerted visual traffic scan could explain why both pilots may not have seen the other aircraft but, without the knowledge of one another's intended operations they lacked situational awareness. Generally, agricultural pilots relied on visual separation and vertical segregation to avoid collisions. In this instance, the proximity of the field being sprayed to the airstrip from which ATB took off and the aircraft's climb gradient from that airstrip, brought the two aircraft into conflict.

Occurrence summary

Investigation number AO-2008-014
Occurrence date 26/02/2008
Location Wee Waa
State New South Wales
Report release date 26/07/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Airborne collision
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Air Tractor Inc
Model AT502
Registration VH-CJK
Serial number 502-0057
Sector Turboprop
Operation type Aerial Work
Departure point ALA 4.5 km SW Wee Waa NSW
Destination ALA 4.5 km SW Wee Waa NSW
Damage Destroyed

Aircraft details

Manufacturer Air Tractor Inc
Model AT502
Registration VH-ATB
Serial number 502B-0287
Sector Turboprop
Operation type Aerial Work
Departure point ALA 13 km NE Wee Waa NSW
Destination ALA 13 km NE Wee Waa NSW
Damage Destroyed

Runway excursion, VH-UZD, Thangool Aerodrome, Queensland, on 12 February 2008

Summary

On 12 February 2008, a Fairchild Industries SA227-AC (Metro III) aircraft, registered VH-UZD, was being operated on a freight service between Emerald and Thangool, Queensland with two pilots. The approach and landing into Thangool were conducted after last light in conditions of scattered low cloud and rain showers. At a speed of about 40 kts after touchdown, the aircraft suddenly veered uncontrollably to the right, departed the runway and became bogged in wet grass.

There was no damage to the aircraft or injuries to the flight crew.

The investigation determined that the runway excursion was probably a result of a directional upset at a time when the nosewheel was in castor mode. The reason for the nosewheel being in the castor mode could not be determined with certainty and may have been the result of an intermittent fault or the inadvertent failure by the flight crew to arm the system.

It was also determined that the aircraft's rate of descent during the latter stages of the approach was significantly higher than for a normal stabilised approach. In addition, the aircraft operator's stabilised approach criteria did not provide flight crew with information on maximum permitted rates of descent. The aircraft operator has advised that, as a result of the investigation, it has redefined its stabilised approach criteria.

Occurrence summary

Investigation number AO-2008-009
Occurrence date 12/02/2008
Location Thangool
State Queensland
Report release date 25/06/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Runway excursion
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Fairchild Industries Inc
Model SA227
Registration VH-UZD
Serial number AC-490
Sector Turboprop
Operation type Charter
Departure point Emerald Qld
Destination Thangool Qld
Damage Nil

Mid-air collision - involving Piper PA-18 Super Cub, VH-OUS and Robinson R44 Raven, VH-ZDP, 54 km north-north-west of Gascoyne Junction, Western Australia, on 13 February 2008

Interim report

Interim factual report released 11 November 2008

On 13 February 2008, a Piper Aircraft Corporation Super Cub aeroplane and a Robinson Helicopter Company R44 Raven helicopter collided in midair during feral goat culling operations. The aeroplane impacted the ground at a steep angle, fatally injuring the two occupants. The helicopter, though damaged, was safely landed.

Preliminary report

Preliminary report released 20 March 2008

On 13 February 2008, a Piper Aircraft Corporation Super Cub aeroplane and a Robinson Helicopter Company R44 Raven helicopter collided in midair during feral goat culling operations. The aeroplane impacted the ground at a steep angle, fatally injuring the two occupants. The helicopter, though damaged, was safely landed.

Summary

On 13 February 2008, a Piper Aircraft Corporation PA-18 Super Cub aircraft and a Robinson Helicopter Company R44 Raven helicopter were engaged in feral goat culling operations in the Kennedy Range National Park, WA.

The two aircraft collided in mid-air as the pilot of the helicopter executed a climbing left turn that brought the two aircraft into close proximity. The pilot and shooter occupants of the R44 were aware that the Super Cub was approaching them at the same height, and the helicopter pilot was aware of the position of the aeroplane during the helicopter's climbing turn, but it appeared probable that the pilot and spotter occupants of the Super Cub did not see the helicopter.

The helicopter's main rotor blades struck the Super Cub's right wing, severing the lift struts. The right wing detached in flight, and the Super Cub fell to the ground. The pilot and spotter were fatally injured. The helicopter was able to land safely.

The investigation determined that the occupants of the Super Cub were probably unaware of the proximity of the R44, and that the R44 pilot did not recognise the collision hazard until there was insufficient time to prevent contact with the Super Cub.

The investigation also identified that there were no formalised operating procedures detailing the conduct of culling operations involving multiple aircraft that may have assisted in the maintenance of aircraft separation.

In response to this accident, a number of safety actions were undertaken by the R44 and Super Cub operators. In addition, extensive safety action was carried out by the WA Government departments that were involved in the operation. That included in the areas of risk management, the review and amendment of guidelines and procedures affecting multiple aircraft operations, the adoption of Safety Management Systems, and the provision of training for departmental personnel.

Inquest

Response to Gascoyne Junction Inquest Findings

On Friday 5 July 2013 the Western Australian (WA) State Coroner released the findings of his investigation into a 2008 fatal Piper Super Cub mid-air collision with a Robinson R44 helicopter 53km north-north-west of Gascoyne Junction. The Australian Transport Safety Bureau (ATSB) has reviewed the Coroner’s findings and reaffirms the safety factors identified by its own investigation. The ATSB’s report was released on 26 June 2009.

ATSB Report

Circumstances of the Accident:

On 13 February 2008, a Piper Aircraft Corporation PA-18 Super Cub aircraft and a Robinson Helicopter Company R44 Raven helicopter were engaged in feral goat culling operations in the Kennedy Range National Park, WA. The operation was initiated by the WA Department of Environment and Conservation (DEC) who contracted the Department of Agriculture and Food, WA (DAF) to assist.

The two aircraft collided in midair as the pilot of the helicopter executed a climbing left turn that brought the two aircraft into close proximity. The pilot and shooter occupants of the R44 were aware that the Super Cub was approaching them at the same height, and the helicopter pilot was aware of the position of the aeroplane during the helicopter's climbing turn, but it appeared probable that the pilot and spotter occupants of the Super Cub did not see the helicopter.

The ATSB found that the Super Cub climbed up and through the disk formed by the helicopter’s rotor blades. The helicopter's main rotor blades struck the Super Cub's right wing, severing the lift struts. The right wing detached in flight, and the Super Cub fell to the ground. The pilot and spotter were fatally injured. The helicopter was able to land safely.

Safety Factors and Key Findings:

In its Final Report the ATSB found the following contributing safety factors:

  • At about the time the two aircraft passed each other, the R44 pilot initiated a climbing left turn that resulted in the two aircraft coming into close proximity;
  • The Super Cub occupants were probably unable to see the R44 during the period beginning at or about the time the helicopter commenced the climbing left turn until the collision;
  • There was no alerting radio call to advise the Super Cub occupants of the R44 position and intentions;
  • Only the R44 pilot was aware of the relative position of the two aircraft;
  • The Super Cub pilot’s manoeuvre resulted in the two aircraft converging;
  • The R44 pilot did not recognise the collision risk until there was insufficient time to prevent contact with the Super Cub;
  • There were no formalised operating procedures detailing the conduct of multiple aircraft culling operations, including the assurance of aircraft separation that would have assisted the pilots maintain separation from each other [safety issue]. 

The ATSB also made a key finding that:

  • The R44 pilot’s work schedule was unlikely to have resulted in work-induced fatigue leading to a significant performance decrement in his ability to operate the helicopter.

Coroner’s Findings

How the accident occurred:

The coroner found that at impact the R44 was rising up into the Super Cub.

The Coroner based this finding on the recollection of the shooter in evidence. In his evidence, the shooter stated that the Super Cub was higher than the R44 as the aircraft passed each other prior to the collision. The Coroner did not consider the ATSB scenario of events likely.

ATSB response:

The ATSB acknowledges the grounds for the Coroner’s finding while reaffirming its assessment that the wing of the Super cub climbed up and passed through the main rotor blade disk of the R44. The ATSB’s assessment was based on the following grounds:

  • The account of the circumstances prior to the collision given by the R44 pilot to the ATSB following the accident. The shooter did not assert that the Super Cub passed higher than the R44. He advised the ATSB that he “recalled last seeing the Super Cub pass to his left at a lower altitude before his attention was diverted inside the helicopter by the movement of the ammunition container” (see ATSB Final Report p.3);
  • The relative bank and pitch between the two aircraft at impact were derived from physical evidence of the contact. The ATSB maintains that the Supercub and the R44 were aligned on a very similar plane at the time of the collision.

Fatigue

The Coroner found that ‘fatigue must have played a significant role’ in both the R44 and Super Cub pilots decision making to allow the aircraft to come into close proximity.

ATSB response

The ATSB reaffirms its finding that:

The R44 pilot’s work schedule was unlikely to have resulted in work-induced fatigue leading to a significant performance decrement in his ability to operate the helicopter.

As part of its investigation the ATSB undertook a fatigue analysis of the R44 pilot. That involved analysing the R44 pilot’s hours worked and his reported rest over the fortnight preceding the accident and on the day of the accident flight. The analysis included examining the pilot’s work and rest periods on the day of the accident using two separate, internationally-accepted bio-mathematical fatigue modelling software programs (FAID and FAST).1

The ATSB was not able to conduct a similar assessment on the Super Cub pilot but it was reported that his workload in the period leading up to the accident was similar to that of the R44 pilot.

Coroner Recommendations: 

The Coroner did not make any recommendations directed toward the ATSB; however the ATSB notes the following recommendations by the Coroner:

  1. That both DEC and DAF put in place guidelines in respect of aerial work which would specifically cover feral animal culling, to ensure that there is at least a 500 foot vertical buffer between spotter and shooter aircraft in addition to any horizontal buffer.
  2. DEC and DAF take action to ensure that ongoing consideration is given to possible use of available anti-collision systems and particularly the FLARM system.

It is not a matter for the ATSB to provide a response to these recommendations. The ATSB considered that the safety issue arising out of this accident that needed to be addressed was the lack of formalised operating procedures detailing the conduct of multiple aircraft culling operations, including the assurance of aircraft separation that would have assisted the pilots maintain separation from each other.

The ATSB report at pp. 29 to 30 details the actions taken or that were planned to be taken in relation to this issue by the:

  • R44 Operator;
  • Super Cub Operator;
  • WA DEC; and
  • DAF WA.

ATSB Investigations and Coronial Inquiries

Inquests are separate to ATSB investigations. The Coroner formulated his findings and recommendations independently of the ATSB. The ATSB cannot speak for the Coroner’s findings. However, the ATSB supports the coronial process and in the interests of ensuring that safety information is made available to the broadest audience the ATSB is making this publication.

The Coroner's report can be obtained from the Coroner's Court of Western Australia. Contact details are available at: www.coronerscourt.wa.gov.au. Queries regarding the Coroner's findings should be directed to the Coroner's Court of Western Australia.

__________________

1 See www.faidsafe.com and  www.fatiguescience.com 

Occurrence summary

Investigation number AO-2008-010
Occurrence date 13/02/2008
Location Kennedy Range National Park
State Western Australia
Report release date 26/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Airborne collision
Occurrence class Accident
Highest injury level Fatal

Aircraft details

Manufacturer Robinson Helicopter Co
Model R-44
Registration VH-ZDP
Serial number 1246
Sector Helicopter
Operation type Aerial Work
Departure point Gascoyne Junction (ALA)
Destination Gascoyne Junction (ALA)
Damage Substantial

Aircraft details

Manufacturer Piper Aircraft Corp
Model PA-18-150
Registration VH-OUS
Serial number 18-7881
Sector Piston
Operation type Aerial Work
Departure point Gascoyne Junction (ALA)
Destination Gascoyne Junction (ALA)
Damage Destroyed

Engine failure – Jabiru, Northern Territory, on 11 February 2008, VH-VAZ, Beech Aircraft 1900

Interim report

Interim Factual report released 22 August 2008

On 11 February 2008 at about 0720 Central Standard Time, following take-off from runway 27 at Jabiru Airport, NT, a Beech Aircraft Corporation 1900D, registered VH-VAZ, sustained an auto-feather of the left propeller and subsequent left engine failure.

The aircraft was being operated on a charter flight to Darwin with two pilots and a passenger on board. The pilots reported that, following the engine failure, they completed a single-engine circuit and landing at Jabiru. Subsequent examination of the left engine revealed catastrophic internal damage to the power section of the engine.

Summary

On 11 February 2008, at about 0720 Central Standard Time, following take-off from runway 27 at Jabiru Airport, NT, a Beech Aircraft Corporation 1900D, registered VH-VAZ, sustained an auto-feather of the left propeller and subsequent left engine failure.

The aircraft was being operated on a charter flight to Darwin with two pilots and a passenger on board. The pilots reported that, following the engine failure, they completed a single-engine circuit and landing at Jabiru. Subsequent examination of the left engine revealed catastrophic internal damage to the power section of the engine. The initiator of the damage was the release of a power turbine second-stage blade. Metallurgical examination determined that the failure of the second-stage turbine blade had occurred as a consequence of the initiation and growth of a high-cycle fatigue cracking mechanism from the downstream trailing corner of the blade fir-tree root post. At the time of blade fracture, approximately 25% of the root cross-section had been compromised by fatigue cracking.

The investigation found that during the most recent overhaul of the engine, the overhaul facility did not comply with the engine manufacturer's service bulletin regarding second-stage turbine blade replacement. Consequently, outdated blades were installed.

Occurrence summary

Investigation number AO-2008-008
Occurrence date 11/02/2008
Location Jabiru Airport
State Northern Territory
Report release date 15/07/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Engine failure or malfunction
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Beech Aircraft Corp
Model 1900
Registration VH-VAZ
Serial number UE-115
Sector Turboprop
Operation type Charter
Departure point Jabiru, NT
Destination Darwin, NT
Damage Nil

Hard landing - Darwin Airport, Northern Territory, on 7 February 2008, VH-NXE, Boeing 717-200

Interim report

Interim report released 11 July 2008

On 7 February 2008, a Boeing Company 717-200 aircraft, registered VH-NXE, was being operated on a scheduled passenger service from Cairns, Qld, via Nhulunbuy (Gove) to Darwin, NT, with six crew and 88 passengers. During an ILS approach to runway 29 at Darwin Airport, the aircraft touched down on the runway at a high rate of descent which resulted in a hard landing. The crew completed the landing rollout and taxied the aircraft to the terminal without further incident. The extent of aircraft damage constituted an accident

Preliminary report

Preliminary report released 27 March 2008

On 7 February 2008, a Boeing Company 717200 aircraft, registered VH-NXE, was being operated on a scheduled passenger service from Cairns, Qld, via Nhulunbuy (Gove) to Darwin, NT, with six crew and 88 passengers. During an ILS approach to runway 29 at Darwin Airport, the aircraft touched down on the runway at a high rate of descent which resulted in a hard landing. The aircraft then bounced before settling onto the runway. The crew completed the landing rollout and taxied the aircraft to the terminal without further incident.

Final report

What happened

On 7 February 2008, a Boeing Company 717-200 aircraft, registered VH-NXE, was being operated on a scheduled passenger service from Cairns, Queensland via Nhulunbuy (Gove) to Darwin, Northern Territory with six crew and 88 passengers.

The flight crew were cleared by air traffic control to fly a visual approach to runway 29 at Darwin Airport and elected to follow the instrument landing system to the runway. The aircraft was above the glideslope for the majority of its approach and temporarily exceeded the operator's stabilised approach criteria shortly before landing. The aircraft sustained a hard landing resulting in structural damage. The flight crew completed the landing roll and taxied the aircraft to the terminal without further incident. There were no reported injuries; however, the extent of the damage to the aircraft led the ATSB to classify the occurrence as an accident. The investigation identified a number of relevant safety factors, including the flight crew's actions and control inputs, the aircraft operator's stabilised approach criteria and operational documentation, and the visual cues associated with runway 11/29 at Darwin Airport.

As a result of this occurrence, the aircraft operator implemented a number of safety actions in relation to enhancing their stabilised approach criteria and pilot training, the monitoring of third-party training providers, and the amendment of relevant operational documentation. In addition, the Civil Aviation Safety Authority (CASA) undertook to prioritise the completion of proposed legislation in relation to third party training providers. In June 2013, CASA advised the ATSB that CASR Part 141 and 142 have now been made and compliance with these regulations will address the safety issue.

Occurrence summary

Investigation number AO-2008-007
Occurrence date 07/02/2008
Location Darwin Airport
State Northern Territory
Report release date 14/05/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Hard landing
Occurrence class Accident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 717
Registration VH-NXE
Serial number 55063
Sector Jet
Operation type Air Transport High Capacity
Departure point Gove, NT
Destination Darwin, NT
Damage Substantial

Breakdown of separation, VH-TQZ, Tamworth Aerodrome, New South Wales, on 7 February 2008

Summary

On 7 February 2008 at Tamworth Aerodrome, New South Wales, an air traffic controller issued a take-off clearance to the flight crew of a Bombardier Inc DHC-8-315 (DHC8) aircraft, registered VH-TQZ, for runway 30 Right. At the same time, an airport operations officer was operating a vehicle on that runway.

The controller had previously issued a clearance to the operations officer to conduct bird dispersal activities on the runway. The operations officer was monitoring his radio and heard the DHC8's take-off clearance. He advised the controller that he would vacate the runway. At the same time, the flight crew had observed the vehicle on the runway and did not commence the takeoff. The controller cancelled the take-off clearance until the runway was clear.

While these secondary safety defences effectively prevented any possibility of an accident, the issue of the take-off clearance with the vehicle on the runway constituted a breakdown of separation.

The investigation found that the controller's scan of the runway and flight strip board was not effective as a result of his pre-occupation with the management of current and pending traffic and the associated high volume of radio communications. It was also possible that the controller was experiencing some degree of fatigue at the time. The ATSB's investigation did not detect any safety issues that required consequent safety action.

Occurrence summary

Investigation number AO-2008-006
Occurrence date 07/02/2008
Location Tamworth
State New South Wales
Report release date 20/08/2010
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Loss of separation
Occurrence class Incident
Highest injury level None

Aircraft details

Manufacturer Bombardier Inc
Model DHC-8
Registration VH-TQZ
Serial number 555
Sector Turboprop
Operation type Air Transport High Capacity
Departure point Tamworth, NSW
Destination Sydney, NSW
Damage Nil

Engine Failure - VH-PSQ, Cessna 208, 15 km west of Townsville Airport, Queensland, on 14 January 2008

Summary

On 14 January 2008 the pilot of a single-engine Cessna Aircraft Company 208 conducted a successful forced landing back onto the departure runway after the aircraft's engine failed. The flight, with six passengers onboard, had earlier departed Townsville, Qld on a private Instrument Flight Rules (IFR) flight to Mt. Isa.

The evidence showed that the failure of the engine was precipitated by the fracture and separation of a single blade from the compressor turbine (CT) disc. The gross mechanical interference caused by the release of that blade into the confines of the turbine section contributed to the subsequent forced fracture of the other CT blades and the downstream migration of blade debris. The remainder of the internal engine damage was identified as secondary damage as a result of that debris.

Damage to the area of crack initiation limited the extent of examination such that the root cause of fatigue initiation could not be established with certainty. However, from the available evidence, it was considered likely that the crack initiated at a localised area of stress concentration, such as may have arisen from the passage of foreign object debris through the engine, from handling or tooling damage sustained during a prior maintenance activity, or from the effects of an isolated blade casting anomaly that was not evident to the examination.

Occurrence summary

Investigation number AO-2008-005
Occurrence date 14/01/2008
Location Townsville Airport
State Queensland
Report release date 05/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Engine failure or malfunction
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer Cessna Aircraft Company
Model 208
Registration VH-PSQ
Serial number 20800213
Operation type Private
Departure point Townsville, Qld
Destination Mount Isa, Qld
Damage Nil

Crew incapacitation, Brisbane Airport, Queensland, on 11 January 2008, VH-OBN, Boeing 737-200

Summary

At approximately 1224 Eastern Standard Time on 11 January 2008, a Boeing 737-200 aircraft, registered VH-OBN, was intercepting the localiser for an instrument landing system approach to runway 01, Brisbane Airport, Qld. The operating crew for the passenger flight included two flight crew (pilot in command (PIC) and copilot) and three cabin crew. The copilot was the handling pilot.

The copilot had reported to the PIC that he was feeling a bit uncomfortable. Shortly after, the copilot handed over control of the aircraft to the PIC and vacated the cockpit due to pain and discomfort.

The PIC continued the approach and landing, without the copilot. Following the landing, as the aircraft entered the taxiway, the copilot returned to the cockpit and resumed support duties until the aircraft reached the gate.

Following the event, the copilot was diagnosed with and received treatment for diverticulitis.

Occurrence summary

Investigation number AO-2008-004
Occurrence date 11/01/2008
Location near Brisbane Airport
State Queensland
Report release date 17/06/2009
Report status Final
Investigation level Systemic
Investigation type Occurrence Investigation
Investigation status Completed
Mode of transport Aviation
Aviation occurrence category Flight crew incapacitation
Occurrence class Serious Incident
Highest injury level None

Aircraft details

Manufacturer The Boeing Company
Model 737
Registration VH-OBN
Serial number 21137
Sector Jet
Operation type Air Transport High Capacity
Departure point Norfolk Island
Destination Brisbane, Qld
Damage Nil